TY  - RPRT
TI  - Optimization problems caused by interaction of guidance and propellant systems.
AU  - Chandler, D. C.
AU  - Horn, H. J.
AU  - Ryan, R. S.
PY  - 1966
UR  - https://ntrs.nasa.gov/citations/19670041246
ID  - 19670041246
ER  -